NTSB CAROL · Event
Event CEN11LA386
Registry · N539ND
FAA Aircraft Registry record.
Make / Model
CESSNA 172S
Year of manufacture
2008 · 3 years old at event
Engine
LYCOMING IO-360-L2A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20081121
ADS-B equipped
Yes — Mode-S A6D30C
Registrant of record
AEROSIM ACADEMY INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The flight instructor’s delayed remedial action to the student pilot’s bounced landing and subsequent loss of aircraft control.
Factual narrative
On June 13, 2011, at 1210 central daylight time, a Cessna model 172S airplane, N539ND, was substantially damaged during a hard landing at Grand Forks International Airport (KGFK), Grand Forks, North Dakota. The flight instructor and student were not injured. The airplane was registered to and operated by the University of North Dakota, under the provisions of 14 Code of Federal Regulations Part 91. Day visual meteorological conditions prevailed for the flight, which was operated without a flight plan. The local instructional flight originated from KGFK at 1110. The flight instructor reported that his student was practicing landings to runway 17R when the accident occurred. The student, who was obtaining instruction toward a flight instructor certificate, was flying from the right seat. The flight instructor reported that the airplane touched down right of the runway centerline and began to bounce as the student attempted to realign the airplane with the centerline. He stated that a wind gust was likely responsible for the initial bounce, but the airplane continued to bounce with an escalating intensity. He noted that on the third or fourth bounce he assumed control of the airplane in order to abort the landing. He reported that before he could establish a climb the airplane experienced an additional hard landing. He regained control and landed the airplane without further incident. A postaccident inspection of the airplane revealed substantial buckling to the firewall. The nose landing gear was displaced 20-30 degrees forward. The operator reported that there were no preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane. At 1153, the airport's automated surface observing system reported the following weather conditions: wind 160 degrees at 22 knots, gusting 27 knots; visibility 10 miles; scattered clouds at 2,300 feet above ground level (agl), broken ceilings 11,000 and 25,000 feet agl; temperature 21 degrees Celsius; dew point 14 degrees Celsius; altimeter setting 29.87 inches of mercury. A peak wind velocity measuring 29 knots from 180 degrees was recorded at 1203. The flight instructor reported that his student was practicing landings, and the airplane touched down right of the runway centerline and began to bounce as the student attempted to realign with the centerline. The flight instructor indicated that a wind gust was likely responsible for the initial bounce, but the airplane continued to bounce with an escalating intensity. He noted that on the third or fourth bounce he assumed control of the airplane in order to abort the landing. He reported that before he could establish a climb the airplane experienced an additional hard landing. He regained control and landed the airplane without further incident. The operator reported that there were no preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation - C
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Student pilot
- C Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2011_CEN11LA386.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗